Dj. Baker et C. Rogers, ANALYSIS AND TESTS OF REINFORCED CARBON-EPOXY FOAM-CORE SANDWICH PANELS WITH CUTOUTS/, Journal of the American Helicopter Society, 43(2), 1998, pp. 120-132
The results of a structurally-efficient minimum-gage shear-panel ape p
resented. The shear-panel design is based on an Integrally stiffened s
yntactic-foam stabilized-skin concept with an all-bias-ply tape constr
uction for the skins. The panels considered in the study were designed
to be buckling resistant up to 100 lbs/in. of shear load and to have
an ultimate strength of 300 lbs/in. The experimental buckling strength
of the reinforced panels is 83 to 90 percent of the predicted bucklin
g strength based on a linear buckling analysis. The maximum experiment
al deflection exceeds the maximum deflection predicted by a nonlinear
analysis by approximately one panel thickness. The failure strength of
the reinforced panels was two and a half to four times the buckling s
trength. This efficient shear-panel design concept exceeds the require
d ultimate strength requirement of 300 lbs/in. by over 100 percent.